Closed-Loop, Exact-Time, Minimum-Energy Attitude Control with Analytic Gain Selection
Author:
Affiliation:
1. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China
2. Polytechnic University of Milan, 20156 Milan, Italy
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Reference31 articles.
1. Precise Attitude Control of Multirotary-Joint Solar-Power Satellite
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